EP3379434A1 - A system and method for design of additively manufactured products - Google Patents

A system and method for design of additively manufactured products Download PDF

Info

Publication number
EP3379434A1
EP3379434A1 EP17203244.3A EP17203244A EP3379434A1 EP 3379434 A1 EP3379434 A1 EP 3379434A1 EP 17203244 A EP17203244 A EP 17203244A EP 3379434 A1 EP3379434 A1 EP 3379434A1
Authority
EP
European Patent Office
Prior art keywords
safety
factor
topology optimization
designing
additive manufacturing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP17203244.3A
Other languages
German (de)
French (fr)
Other versions
EP3379434B1 (en
Inventor
Pramod Ramdas ZAGADE
Purushottham Gautham BASAVARSU
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tata Consultancy Services Ltd
Original Assignee
Tata Consultancy Services Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Tata Consultancy Services Ltd filed Critical Tata Consultancy Services Ltd
Publication of EP3379434A1 publication Critical patent/EP3379434A1/en
Application granted granted Critical
Publication of EP3379434B1 publication Critical patent/EP3379434B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/17Mechanical parametric or variational design
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06TIMAGE DATA PROCESSING OR GENERATION, IN GENERAL
    • G06T17/00Three dimensional [3D] modelling, e.g. data description of 3D objects
    • G06T17/20Finite element generation, e.g. wire-frame surface description, tesselation
    • G06T17/205Re-meshing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C64/00Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
    • B29C64/30Auxiliary operations or equipment
    • B29C64/386Data acquisition or data processing for additive manufacturing
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation
    • G06F30/23Design optimisation, verification or simulation using finite element methods [FEM] or finite difference methods [FDM]
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F2113/00Details relating to the application field
    • G06F2113/10Additive manufacturing, e.g. 3D printing
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F2119/00Details relating to the type or aim of the analysis or the optimisation
    • G06F2119/18Manufacturability analysis or optimisation for manufacturability
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P90/00Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
    • Y02P90/02Total factory control, e.g. smart factories, flexible manufacturing systems [FMS] or integrated manufacturing systems [IMS]

Definitions

  • the embodiments herein generally relates to a system and method for obtaining topologically optimized structure in additive manufacturing and, more particularly, determining optimal shape and build orientation of a structure having anisotropic properties induced due to additive manufacturing.
  • additive manufacturing is a rapidly emerging technology to produce parts having complex shapes. It uses layer-by-layer deposition of material to build three dimensional structures. Ideally there are no limitations on the geometry of parts that can be produced using additive manufacturing technology. It offers a great freedom to designers to design products of any complex shape with least possible amount of material and target of minimum weight to achieve required functionality.
  • layered structure leads to anisotropy in the material with different mechanical properties along various directions. The difference in mechanical properties such as yield strength along built and lateral directions is significant. It imposes constraints on the designers, as they have to consider strength in the weakest direction as design norm while evaluating safety of the designed structure. On the other hand, heat treatments are often essential and used for these parts to homogenize the properties.
  • Parts are heated to a higher temperature and held for some time to introduce microstructural changes in the part and are then cooled in a controlled environment. As a result of heat treatment, microstructural changes take place. It reduces the inhomogeneity of properties in the part, but most of the time at the expense of strength and yet not fully alleviating anisotropy. Addressing anisotropic properties may also require decisions on optimum build orientation while manufacturing the part at the design stage itself. Existing guidelines on how the part should be oriented while manufacturing additively are based on dimensions of the part, support structure design and machine specifications.
  • topology optimization is performed with a computer system and generally divided into sizing, shape and topology.
  • the application of topology optimization is the best suited technique to design such parts having minimal manufacturing constraints such as those produced using additive manufacturing.
  • Topology optimization used for designing the structural part should consider the anisotropic properties it may possess after being produced through additive manufacturing.
  • an embodiment herein provides a system and method for obtaining topologically optimized structure manufactured by additive manufacturing processes.
  • a system for obtaining topologically optimized structure to be manufactured by additive manufacturing processes comprises a processor, a memory communicatively coupled to the processor and the memory contains instructions that are readable by the processor, a receiver module is configured to receive a finite element mesh of a standard shape geometry encompassing desired structure to be optimized in accordance with at least one design objective and orthotropic properties of material arising out of a selected material and selected additive manufacturing process to be used for manufacturing the designed structure, an application module is configured to apply an iterative topology optimization of the designing structure, wherein each iteration of the topology optimization comprising of simulating one or more loading requirements, one or more design constraints and one or more boundary conditions under which the designing structure is designed and optimized, an evaluation module is configured to evaluate the designing structure resulted from application of the iterative topology optimization using finite element analysis framework to obtain a predefined factor of safety based on the anisotropic properties of the material arising out of the selected additive manufacturing process, wherein the predefined factor of safety condition is defined as a
  • a method for obtaining topologically optimized structure in additive manufacturing comprises receiving a finite element mesh of a standard shape geometry encompassing desired structure to be optimized in accordance with at least one design objective and orthotropic properties of material arising out of a selected material and selected additive manufacturing process to be used for manufacturing the designed structure applying an iterative topology optimization of the designing structure, wherein each iteration of the topology optimization comprising of simulating one or more loading requirements, one or more design constraints and one or more boundary conditions under which the designing structure is designed and optimized, evaluating the designing structure resulted from application of the iterative topology optimization using finite element analysis framework to obtain a predefined factor of safety based on the anisotropic properties of the material arising out of the selected additive manufacturing process, wherein the predefined factor of safety condition is defined as a substantially small difference in comparison with evaluated factor of safety modifying the state of the finite element iteratively according to one or more changes of the factor of safety between two consecutive iterations of the iterative topology optimization of the designing
  • any block diagram herein represent conceptual views of illustrative systems embodying the principles of the present subject matter.
  • any flow charts, flow diagrams, state transition diagrams, pseudo code, and the like represent various processes which may be substantially represented in computer readable medium and so executed by a computing device or processor, whether or not such computing device or processor is explicitly shown.
  • a system 100 for obtaining topologically optimized structure in additive manufacturing comprising a processor 102, a memory 104 communicatively coupled to the processor 102, a receiving module 106, an application module 108, an evaluation module 110 and a modification module 112.
  • the memory 104 contains instructions that are readable by the processor 102.
  • the receiver module 106 is configured to receive a finite element mesh of a standard shape geometry encompassing desired structure to be optimized in accordance with at least one design objective and orthotropic properties of material arising out of a selected material and selected additive manufacturing process to be used for manufacturing the designed structure.
  • the application module 108 is configured to apply an iterative topology optimization of the designing structure, wherein each iteration of the topology optimization comprising of simulating one or more loading requirements, one or more design constraints and one or more boundary conditions under which the designing structure is designed and optimized.
  • each iteration of the topology optimization comprising of simulating one or more loading requirements, one or more design constraints and one or more boundary conditions under which the designing structure is designed and optimized.
  • the iteration topology optimization has been performed with Bidirectional Evolutionary Structural Optimization (BESO) process. It would be appreciated that the said disclosure is not limited to the BESO process and can be performed with other topology optimization process.
  • BESO Bidirectional Evolutionary Structural Optimization
  • initially directional properties are assigned to the domain of interest which is a conservative design.
  • a factor of safety concept is being used for structural analysis. The factor of safety is used to determine elemental sensitivity numbers. It is then converted to the nodal sensitivity numbers for the given domain.
  • topology optimization is sensitive to the mesh sizes.
  • a mesh-independency filter using nodal variables is used to determine the utility of the elements. These utility numbers then used as basis and for addition or elimination of elements.
  • the factor of safety based criterion is utilized for defining material removal/addition and termination criteria.
  • the factor of safety is greater than or equal to the predefined minimum factor of safety then element removal and addition activities is activated.
  • the elements are soft killed, by simply reducing their stiffness to a very low value.
  • the evaluation module 110 is configured to evaluate the designing structure resulted from application of the iterative topology optimization using finite element analysis framework to obtain a minimal predefined factor of safety based on the anisotropic properties of the material arising out of the selected additive manufacturing process, wherein the predefined factor of safety condition is defined as a substantially small difference in comparison with evaluated factor of safety. After the one or more iterations once the predefined criteria is met the process is terminated and the optimized structure is saved.
  • topology optimization exercise can be repeated with a set of material properties which may be the result of various additive manufacturing build directions.
  • a predefined criteria for selecting best build direction are based on weight of structure, failure criteria etc.
  • the one or more build orientations are ranked to choose best suitable build orientation when each of them evaluated against the one or more criteria for example, but not limited to, minimum volume, weight or deflection etc.
  • a method 200 for obtaining topologically optimized structure in additive manufacturing is shown.
  • step 202 where the process receives a finite element mesh of a standard shape geometry encompassing desired structure to be optimized in accordance with at least one design objective and orthotropic properties of material arising out of a selected material and selected additive manufacturing process to be used for manufacturing the designed structure.
  • step 204 where the application module applies an iterative topology optimization of the designing structure, wherein each iteration of the topology optimization comprising of simulating one or more loading requirements, one or more design constraints and one or more boundary conditions under which the designing structure is designed and optimized.
  • the evaluation module evaluates the designed structure resulted from application of the iterative topology optimization using finite element analysis framework to obtain a predefined factor of safety based on the anisotropic properties of the material arising out of the selected additive manufacturing process, wherein the predefined factor of safety condition is defined as a substantially small difference in comparison with evaluated factor of safety.
  • the process obtains an optimal design structure for one or more build orientations with information of respective anisotropic properties.
  • the optimal design structure is selected when the entire structure has a minimal factor of safety equivalent to a predefined factor of safety.
  • the one or more build orientations are ranked to choose the best suitable build orientation when each of them evaluated against the one or more criteria for example minimum volume, weight or deflection etc.
  • FIG 3 an example, which illustrates the results after applying proposed method. It shows resulting optimal structures for assumption of varying build direction. E.g. if considered 0° build direction, it corresponds to vertical direction coinciding with build direction and properties are assumed accordingly. Topology optimization algorithm with anisotropic properties and factor of safety based criteria for evolution of structure resulted in an optimal structure. Then it is assumed that build direction is changed and rotated through 22.5°. Material anisotropy parameters are then calculated using appropriate mathematical transformation and corresponding optimal structure is obtained. Such exercise is repeated for 9 representative directions and corresponding optimal structures are shown in the figure. In each case key parameters such as final structure volume and deflection observed after applying load are shown in the form of bar chart. Designer can decide the best possible structure and choose suitable build direction after examining various final shapes and corresponding values of volume and deflection.
  • FIG. 5 illustrates an example of three dimensional optimal structure and key result variables of bracket for varying build orientations.
  • the proposed method can be used for optimization of three dimensional structures as well.
  • build direction variation is considered with respect to all three directions and corresponding results are reported.
  • a system and method to obtain a topologically optimized structure in additive manufacturing A finite element mesh of a standard shape geometry encompassing desired structure to be optimized with a design objective and orthotropic properties of material arising out of a selected material and selected additive manufacturing process to be used for manufacturing.
  • An iterative topology optimization is carried out wherein the process includes simulation of loading requirements, design constraints and the boundary condition.
  • the performance evaluation process uses a finite element analysis framework to obtain the factor of safety between two consecutive iterations based on the anisotropic properties of the material. The process will achieve a minimal factor of safety and a best suitable build orientation of the design.
  • the embodiments of present disclosure herein addresses unresolved problem of anisotropy being introduced in the part of design structure while carrying additive manufacturing process.
  • the anisotropy is commonly observed in metallic part of the design structure.
  • the difference in mechanical properties such as yield strength along built direction is significant. It may lead in heavier parts as such designs are overdesigned in other directions.
  • heat treatment are often suggested and used for such parts so as to have isotropic properties. However, the heat treatment develops microstructural changes which leads to homogenized properties but this causes reduction in overall strength of the material.
  • the hardware device can be any kind of device which can be programmed including e.g. any kind of computer like a server or a personal computer, or the like, or any combination thereof.
  • the device may also include means which could be e.g. hardware means like e.g. an application-specific integrated circuit (ASIC), a field-programmable gate array (FPGA), or a combination of hardware and software means, e.g.
  • ASIC application-specific integrated circuit
  • FPGA field-programmable gate array
  • the means can include both hardware means and software means.
  • the method embodiments described herein could be implemented in hardware and software.
  • the device may also include software means.
  • the embodiments may be implemented on different hardware devices, e.g. using a plurality of CPUs.
  • the embodiments herein can comprise hardware and software elements.
  • the embodiments that are implemented in software include but are not limited to, firmware, resident software, microcode, etc.
  • the functions performed by various modules described herein may be implemented in other modules or combinations of other modules.
  • a computer-usable or computer readable medium can be any apparatus that can comprise, store, communicate, propagate, or transport the program for use by or in connection with the instruction execution system, apparatus, or device.
  • the medium can be an electronic, magnetic, optical, electromagnetic, infrared, or semiconductor system (or apparatus or device) or a propagation medium.
  • Examples of a computer-readable medium include a semiconductor or solid state memory, magnetic tape, a removable computer diskette, a random access memory (RAM), a read-only memory (ROM), a rigid magnetic disk and an optical disk.
  • Current examples of optical disks include compact disk-read only memory (CD-ROM), compact disk-read/write (CD-R/W) and DVD.
  • a data processing system suitable for storing and/or executing program code will include at least one processor coupled directly or indirectly to memory elements through a system bus.
  • the memory elements can include local memory employed during actual execution of the program code, bulk storage, and cache memories which provide temporary storage of at least some program code in order to reduce the number of times code must be retrieved from bulk storage during execution.
  • I/O devices can be coupled to the system either directly or through intervening I/O controllers.
  • Network adapters may also be coupled to the system to enable the data processing system to become coupled to other data processing systems or remote printers or storage devices through intervening private or public networks. Modems, cable modem and Ethernet cards are just a few of the currently available types of network adapters.
  • a representative hardware environment for practicing the embodiments may include a hardware configuration of an information handling/computer system in accordance with the embodiments herein.
  • the system herein comprises at least one processor or central processing unit (CPU).
  • the CPUs are interconnected via system bus to various devices such as a random access memory (RAM), read-only memory (ROM), and an input/output (I/O) adapter.
  • RAM random access memory
  • ROM read-only memory
  • I/O input/output
  • the I/O adapter can connect to peripheral devices, such as disk units and tape drives, or other program storage devices that are readable by the system.
  • the system can read the inventive instructions on the program storage devices and follow these instructions to execute the methodology of the embodiments herein.
  • the system further includes a user interface adapter that connects a keyboard, mouse, speaker, microphone, and/or other user interface devices such as a touch screen device (not shown) to the bus to gather user input.
  • a communication adapter connects the bus to a data processing network
  • a display adapter connects the bus to a display device which may be embodied as an output device such as a monitor, printer, or transmitter, for example.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Computer Hardware Design (AREA)
  • Evolutionary Computation (AREA)
  • Materials Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Mathematical Optimization (AREA)
  • Pure & Applied Mathematics (AREA)
  • Mathematical Analysis (AREA)
  • Computational Mathematics (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Optics & Photonics (AREA)
  • Computer Graphics (AREA)
  • Software Systems (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)
  • Powder Metallurgy (AREA)

Abstract

A system and method for obtaining topologically optimized structure in additive manufacturing. A finite element mesh of a standard shape geometry encompassing desired structure to be optimized with a design objective and orthotropic properties of material arising out of a selected material and selected additive manufacturing process to be used for manufacturing. An iterative topology optimization is carried out wherein the process includes simulation of loading requirements, design constraints and the boundary condition. The performance evaluation process uses a finite element analysis framework to obtain the factor of safety between two consecutive iterations based on the anisotropic properties of the material. The process will achieve a minimal factor of safety and a best suitable build orientation of the design.

Description

    PRIORITY
  • The present invention claims priority to India Application (Title: A system and method for design of additively manufactured products) No. 201721010130 , filed in India on March 22, 2017.
  • FIELD OF THE INVENTION
  • The embodiments herein generally relates to a system and method for obtaining topologically optimized structure in additive manufacturing and, more particularly, determining optimal shape and build orientation of a structure having anisotropic properties induced due to additive manufacturing.
  • BACKGROUND
  • Today, additive manufacturing is a rapidly emerging technology to produce parts having complex shapes. It uses layer-by-layer deposition of material to build three dimensional structures. Ideally there are no limitations on the geometry of parts that can be produced using additive manufacturing technology. It offers a great freedom to designers to design products of any complex shape with least possible amount of material and target of minimum weight to achieve required functionality. However, in metallic applications, layered structure leads to anisotropy in the material with different mechanical properties along various directions. The difference in mechanical properties such as yield strength along built and lateral directions is significant. It imposes constraints on the designers, as they have to consider strength in the weakest direction as design norm while evaluating safety of the designed structure. On the other hand, heat treatments are often essential and used for these parts to homogenize the properties. Parts are heated to a higher temperature and held for some time to introduce microstructural changes in the part and are then cooled in a controlled environment. As a result of heat treatment, microstructural changes take place. It reduces the inhomogeneity of properties in the part, but most of the time at the expense of strength and yet not fully alleviating anisotropy. Addressing anisotropic properties may also require decisions on optimum build orientation while manufacturing the part at the design stage itself. Existing guidelines on how the part should be oriented while manufacturing additively are based on dimensions of the part, support structure design and machine specifications.
  • Traditionally, design optimization is performed with a computer system and generally divided into sizing, shape and topology. The application of topology optimization is the best suited technique to design such parts having minimal manufacturing constraints such as those produced using additive manufacturing. Topology optimization used for designing the structural part should consider the anisotropic properties it may possess after being produced through additive manufacturing.
  • SUMMARY OF THE INVENTION
  • The following presents a simplified summary of some embodiments of the disclosure in order to provide a basic understanding of the embodiments. This summary is not an extensive overview of the embodiments. It is not intended to identify key/critical elements of the embodiments or to delineate the scope of the embodiments. Its sole purpose is to present some embodiments in a simplified form as a prelude to the more detailed description that is presented below.
  • In view of the foregoing, an embodiment herein provides a system and method for obtaining topologically optimized structure manufactured by additive manufacturing processes.
  • In one aspect, a system for obtaining topologically optimized structure to be manufactured by additive manufacturing processes. The system comprises a processor, a memory communicatively coupled to the processor and the memory contains instructions that are readable by the processor, a receiver module is configured to receive a finite element mesh of a standard shape geometry encompassing desired structure to be optimized in accordance with at least one design objective and orthotropic properties of material arising out of a selected material and selected additive manufacturing process to be used for manufacturing the designed structure, an application module is configured to apply an iterative topology optimization of the designing structure, wherein each iteration of the topology optimization comprising of simulating one or more loading requirements, one or more design constraints and one or more boundary conditions under which the designing structure is designed and optimized, an evaluation module is configured to evaluate the designing structure resulted from application of the iterative topology optimization using finite element analysis framework to obtain a predefined factor of safety based on the anisotropic properties of the material arising out of the selected additive manufacturing process, wherein the predefined factor of safety condition is defined as a substantially small difference in comparison with evaluated factor of safety and a modification module is configured to modify the state of the finite element iteratively according to one or more changes of the factor of safety between two consecutive iterations of the iterative topology optimization of the designing structure and obtaining an optimal designing structure when the entire structure has a minimal factor of safety equivalent to a predefined factor of safety.
  • In another aspect, a method for obtaining topologically optimized structure in additive manufacturing. The method comprises receiving a finite element mesh of a standard shape geometry encompassing desired structure to be optimized in accordance with at least one design objective and orthotropic properties of material arising out of a selected material and selected additive manufacturing process to be used for manufacturing the designed structure applying an iterative topology optimization of the designing structure, wherein each iteration of the topology optimization comprising of simulating one or more loading requirements, one or more design constraints and one or more boundary conditions under which the designing structure is designed and optimized, evaluating the designing structure resulted from application of the iterative topology optimization using finite element analysis framework to obtain a predefined factor of safety based on the anisotropic properties of the material arising out of the selected additive manufacturing process, wherein the predefined factor of safety condition is defined as a substantially small difference in comparison with evaluated factor of safety modifying the state of the finite element iteratively according to one or more changes of the factor of safety between two consecutive iterations of the iterative topology optimization of the designing structure and obtaining an optimal designing structure when the entire structure has a minimal factor of safety equivalent to a predefined factor of safety.
  • It should be appreciated by those skilled in the art that any block diagram herein represent conceptual views of illustrative systems embodying the principles of the present subject matter. Similarly, it will be appreciated that any flow charts, flow diagrams, state transition diagrams, pseudo code, and the like represent various processes which may be substantially represented in computer readable medium and so executed by a computing device or processor, whether or not such computing device or processor is explicitly shown.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The embodiments herein will be better understood from the following detailed description with reference to the drawings, in which:
    • Figure 1 illustrates a system for obtaining topologically optimized structure in additive manufacturing according to an embodiment of the present disclosure;
    • Figure 2 illustrates a method for obtaining topologically optimized structure in additive manufacturing according to an embodiment of the present disclosure;
    • Figure 3 illustrates an example of the optimal structures and key result variables obtained through BESO for directional properties according to an embodiment of the present disclosure;
    • Figure 4 illustrate an example of a control arm optimal structure and key result variables with varying build orientations according to an embodiment of the present disclosure; and
    • Figure 5 illustrate an example of three dimensional optimal structure and key result variables of bracket for varying build orientations according to embodiment of the present disclosure.
    DETAILED DESCRIPTION OF THE INVENTION
  • The embodiments herein and the various features and advantageous details thereof are explained more fully with reference to the non-limiting embodiments that are illustrated in the accompanying drawings and detailed in the following description. The examples used herein are intended merely to facilitate an understanding of ways in which the embodiments herein may be practiced and to further enable those of skill in the art to practice the embodiments herein. Accordingly, the examples should not be construed as limiting the scope of the embodiments herein.
  • Referring fig. 1, a system 100 for obtaining topologically optimized structure in additive manufacturing. The system 100 comprising a processor 102, a memory 104 communicatively coupled to the processor 102, a receiving module 106, an application module 108, an evaluation module 110 and a modification module 112.
  • In the preferred embodiment, the memory 104 contains instructions that are readable by the processor 102.
  • In the preferred embodiment, the receiver module 106 is configured to receive a finite element mesh of a standard shape geometry encompassing desired structure to be optimized in accordance with at least one design objective and orthotropic properties of material arising out of a selected material and selected additive manufacturing process to be used for manufacturing the designed structure.
  • In the preferred embodiment, the application module 108 is configured to apply an iterative topology optimization of the designing structure, wherein each iteration of the topology optimization comprising of simulating one or more loading requirements, one or more design constraints and one or more boundary conditions under which the designing structure is designed and optimized. In the application module 108 the iteration topology optimization has been performed with Bidirectional Evolutionary Structural Optimization (BESO) process. It would be appreciated that the said disclosure is not limited to the BESO process and can be performed with other topology optimization process.
  • In the preferred embodiment, initially directional properties are assigned to the domain of interest which is a conservative design. A factor of safety concept is being used for structural analysis. The factor of safety is used to determine elemental sensitivity numbers. It is then converted to the nodal sensitivity numbers for the given domain. Sometimes, topology optimization is sensitive to the mesh sizes. Hence, a mesh-independency filter using nodal variables is used to determine the utility of the elements. These utility numbers then used as basis and for addition or elimination of elements.
  • Further, it is observed that the output part of structure of conventional process of additive manufacturing will have anisotropy in Young's modulus. Therefore, anisotropy may affect linear deformation behavior in the respective directions. This needs to be accounted for along with anisotropy in the yield strengths in the output part of additive manufacturing. The factor of safety based criterion is utilized for defining material removal/addition and termination criteria. For two dimensional transversely isotropic material, the factor of safety (FOS) is determined using Tsi-Hill criteria: FOS = 1 σ 1 σ 1 ˜ 2 + σ 2 σ 2 ˜ 2 + σ 12 σ 12 ˜ 2 σ 1 σ 2 σ 1 ˜ 2 / 2 1
    Figure imgb0001
    • σ 2 is the stress in build direction
    • σ 1 is the stress in other direction
    • σ̃i is the yield stress in the respective direction
  • Further, if the factor of safety is greater than or equal to the predefined minimum factor of safety then element removal and addition activities is activated. The elements are soft killed, by simply reducing their stiffness to a very low value.
  • In the preferred embodiment, the evaluation module 110 is configured to evaluate the designing structure resulted from application of the iterative topology optimization using finite element analysis framework to obtain a minimal predefined factor of safety based on the anisotropic properties of the material arising out of the selected additive manufacturing process, wherein the predefined factor of safety condition is defined as a substantially small difference in comparison with evaluated factor of safety. After the one or more iterations once the predefined criteria is met the process is terminated and the optimized structure is saved.
  • It would be appreciated that the topology optimization exercise can be repeated with a set of material properties which may be the result of various additive manufacturing build directions. A predefined criteria for selecting best build direction are based on weight of structure, failure criteria etc. Further, the one or more build orientations are ranked to choose best suitable build orientation when each of them evaluated against the one or more criteria for example, but not limited to, minimum volume, weight or deflection etc.
  • Referring fig 2, a method 200 for obtaining topologically optimized structure in additive manufacturing.
  • At step 202, where the process receives a finite element mesh of a standard shape geometry encompassing desired structure to be optimized in accordance with at least one design objective and orthotropic properties of material arising out of a selected material and selected additive manufacturing process to be used for manufacturing the designed structure.
  • At step 204, where the application module applies an iterative topology optimization of the designing structure, wherein each iteration of the topology optimization comprising of simulating one or more loading requirements, one or more design constraints and one or more boundary conditions under which the designing structure is designed and optimized.
  • At step 206, where the evaluation module evaluates the designed structure resulted from application of the iterative topology optimization using finite element analysis framework to obtain a predefined factor of safety based on the anisotropic properties of the material arising out of the selected additive manufacturing process, wherein the predefined factor of safety condition is defined as a substantially small difference in comparison with evaluated factor of safety.
  • At step 208, where the process modifies the state of the finite element iteratively according to one or more changes of the factor of safety between two consecutive iterations of the iterative topology optimization of the designing structure.
  • At final step 210 and 212, where the process obtains an optimal design structure for one or more build orientations with information of respective anisotropic properties. The optimal design structure is selected when the entire structure has a minimal factor of safety equivalent to a predefined factor of safety. Further, the one or more build orientations are ranked to choose the best suitable build orientation when each of them evaluated against the one or more criteria for example minimum volume, weight or deflection etc.
  • In an example, the proposed method is explained with the help of three representative implementations:
    1. a) A two dimensional design of bracket structure to support vertical load;
    2. b) A control lever arm design; and
    3. c) A three dimensional design of bracket structure. For each of the case study, anisotropic properties of material were assumed as follows.
    Property Build up direction in layer direction
    Young's Modulus 151 GPa 156 GPa
    Yield Strength 1170 Mpa 1033 MPa
  • Referring figure 3, an example, which illustrates the results after applying proposed method. It shows resulting optimal structures for assumption of varying build direction. E.g. if considered 0° build direction, it corresponds to vertical direction coinciding with build direction and properties are assumed accordingly. Topology optimization algorithm with anisotropic properties and factor of safety based criteria for evolution of structure resulted in an optimal structure. Then it is assumed that build direction is changed and rotated through 22.5°. Material anisotropy parameters are then calculated using appropriate mathematical transformation and corresponding optimal structure is obtained. Such exercise is repeated for 9 representative directions and corresponding optimal structures are shown in the figure. In each case key parameters such as final structure volume and deflection observed after applying load are shown in the form of bar chart. Designer can decide the best possible structure and choose suitable build direction after examining various final shapes and corresponding values of volume and deflection.
  • Similar approach is repeated for another case study of control arm design, wherein more than one load points are considered. Under such scenario optimal structures in case of varying build direction and corresponding key parameters are shown in fig. 4.
  • Referring fig. 5, illustrates an example of three dimensional optimal structure and key result variables of bracket for varying build orientations. Herein the proposed method can be used for optimization of three dimensional structures as well. In this case build direction variation is considered with respect to all three directions and corresponding results are reported.
  • The written description describes the subject matter herein to enable any person skilled in the art to make and use the embodiments. The scope of the subject matter embodiments is defined by the claims and may include other modifications that occur to those skilled in the art. Such other modifications are intended to be within the scope of the claims if they have similar elements that do not differ from the literal language of the claims or if they include equivalent elements with insubstantial differences from the literal language of the claims.
  • A system and method to obtain a topologically optimized structure in additive manufacturing. A finite element mesh of a standard shape geometry encompassing desired structure to be optimized with a design objective and orthotropic properties of material arising out of a selected material and selected additive manufacturing process to be used for manufacturing. An iterative topology optimization is carried out wherein the process includes simulation of loading requirements, design constraints and the boundary condition. The performance evaluation process uses a finite element analysis framework to obtain the factor of safety between two consecutive iterations based on the anisotropic properties of the material. The process will achieve a minimal factor of safety and a best suitable build orientation of the design.
  • The embodiments of present disclosure herein addresses unresolved problem of anisotropy being introduced in the part of design structure while carrying additive manufacturing process. The anisotropy is commonly observed in metallic part of the design structure. The difference in mechanical properties such as yield strength along built direction is significant. It may lead in heavier parts as such designs are overdesigned in other directions. On the other hand heat treatment are often suggested and used for such parts so as to have isotropic properties. However, the heat treatment develops microstructural changes which leads to homogenized properties but this causes reduction in overall strength of the material.
  • It is, however to be understood that the scope of the protection is extended to such a program and in addition to a computer-readable means having a message therein; such computer-readable storage means contain program-code means for implementation of one or more steps of the method, when the program runs on a server or mobile device or any suitable programmable device. The hardware device can be any kind of device which can be programmed including e.g. any kind of computer like a server or a personal computer, or the like, or any combination thereof. The device may also include means which could be e.g. hardware means like e.g. an application-specific integrated circuit (ASIC), a field-programmable gate array (FPGA), or a combination of hardware and software means, e.g. an ASIC and an FPGA, or at least one microprocessor and at least one memory with software modules located therein. Thus, the means can include both hardware means and software means. The method embodiments described herein could be implemented in hardware and software. The device may also include software means. Alternatively, the embodiments may be implemented on different hardware devices, e.g. using a plurality of CPUs.
  • The embodiments herein can comprise hardware and software elements. The embodiments that are implemented in software include but are not limited to, firmware, resident software, microcode, etc. The functions performed by various modules described herein may be implemented in other modules or combinations of other modules. For the purposes of this description, a computer-usable or computer readable medium can be any apparatus that can comprise, store, communicate, propagate, or transport the program for use by or in connection with the instruction execution system, apparatus, or device.
  • The medium can be an electronic, magnetic, optical, electromagnetic, infrared, or semiconductor system (or apparatus or device) or a propagation medium. Examples of a computer-readable medium include a semiconductor or solid state memory, magnetic tape, a removable computer diskette, a random access memory (RAM), a read-only memory (ROM), a rigid magnetic disk and an optical disk. Current examples of optical disks include compact disk-read only memory (CD-ROM), compact disk-read/write (CD-R/W) and DVD.
  • A data processing system suitable for storing and/or executing program code will include at least one processor coupled directly or indirectly to memory elements through a system bus. The memory elements can include local memory employed during actual execution of the program code, bulk storage, and cache memories which provide temporary storage of at least some program code in order to reduce the number of times code must be retrieved from bulk storage during execution.
  • Input/output (I/O) devices (including but not limited to keyboards, displays, pointing devices, etc.) can be coupled to the system either directly or through intervening I/O controllers. Network adapters may also be coupled to the system to enable the data processing system to become coupled to other data processing systems or remote printers or storage devices through intervening private or public networks. Modems, cable modem and Ethernet cards are just a few of the currently available types of network adapters.
  • A representative hardware environment for practicing the embodiments may include a hardware configuration of an information handling/computer system in accordance with the embodiments herein. The system herein comprises at least one processor or central processing unit (CPU). The CPUs are interconnected via system bus to various devices such as a random access memory (RAM), read-only memory (ROM), and an input/output (I/O) adapter. The I/O adapter can connect to peripheral devices, such as disk units and tape drives, or other program storage devices that are readable by the system. The system can read the inventive instructions on the program storage devices and follow these instructions to execute the methodology of the embodiments herein.
  • The system further includes a user interface adapter that connects a keyboard, mouse, speaker, microphone, and/or other user interface devices such as a touch screen device (not shown) to the bus to gather user input. Additionally, a communication adapter connects the bus to a data processing network, and a display adapter connects the bus to a display device which may be embodied as an output device such as a monitor, printer, or transmitter, for example.
  • The preceding description has been presented with reference to various embodiments. Persons having ordinary skill in the art and technology to which this application pertains will appreciate that alterations and changes in the described structures and methods of operation can be practiced without meaningfully departing from the principle, spirit and scope.

Claims (8)

  1. A method for obtaining topologically optimized structure in additive manufacturing, the method comprising:
    receiving, at a receiver module, a finite element mesh of a standard shape geometry encompassing desired structure to be optimized in accordance with at least one design objective and orthotropic properties of material arising out of a selected material and selected additive manufacturing process to be used for manufacturing the designed structure;
    applying, at an application module, an iterative topology optimization of the designing structure, wherein each iteration of the topology optimization comprising of simulating one or more loading requirements, one or more design constraints and one or more boundary conditions under which the designing structure is designed and optimized;
    evaluating, at an evaluation module, the designing structure resulted from application of the iterative topology optimization using finite element analysis framework to obtain a predefined factor of safety based on the anisotropic properties of the material arising out of the selected additive manufacturing process, wherein the predefined factor of safety condition is defined as a substantially small difference in comparison with evaluated factor of safety;
    modifying, at a modification module, the state of the finite element iteratively according to one or more changes of the factor of safety between two consecutive iterations of the iterative topology optimization of the designing structure; and
    obtaining an optimal designing structure when the entire structure has a minimal factor of safety equivalent to a predefined factor of safety.
  2. The method claimed in claim 1, wherein the method further applied to obtain optimal designed structures for one or more build orientations with information of respective anisotropic properties.
  3. The method claimed in claim 2, wherein the one or more build orientations are ranked to obtain a build orientation when evaluated against one or more criteria.
  4. The method claimed in claim 1, wherein the iterative topology optimization includes bidirectional evolutionary structural optimization (BESO).
  5. A system for obtaining topologically optimized structure in additive manufacturing, the system comprising:
    a memory having one or more computer readable instructions;
    at least one processor communicatively coupled with the memory, wherein the at least one processor executing one or more instructions stored in the memory;
    a receiver module is configured to receive a finite element mesh of a standard shape geometry encompassing desired structure to be optimized in accordance with at least one design objective and orthotropic properties of material arising out of a selected material and selected additive manufacturing process to be used for manufacturing the designed structure;
    an application module is configured to apply an iterative topology optimization of the designing structure, wherein each iteration of the topology optimization comprising of simulating one or more loading requirements, one or more design constraints and one or more boundary conditions under which the designing structure is designed and optimized;
    an evaluation module is configured to evaluate the designing structure resulted from application of the iterative topology optimization using finite element analysis framework to obtain a predefined factor of safety based on the anisotropic properties of the material arising out of the selected additive manufacturing process, wherein the predefined factor of safety condition is defined as a substantially small difference in comparison with evaluated factor of safety;
    a modification module is configured to modify the state of the finite element iteratively according to one or more changes of the factor of safety between two consecutive iterations of the iterative topology optimization of the designing structure; and
    obtaining an optimal designing structure when the entire structure has a minimal factor of safety equivalent to a predefined factor of safety.
  6. The system claimed in claim 5, wherein the at least one design objective includes fitment of each of the finite elements of the designing structure by keeping a predefined mass and stress of the designing structure.
  7. The system claimed in claim 5, wherein the iterative topology optimization includes bidirectional evolutionary structural optimization (BESO).
  8. A non-transitory computer readable medium storing one or more instructions which when executed by a processor on a system, cause the processor to perform method for obtaining topologically optimized structure in additive manufacturing comprising:
    receiving, at a receiver module, a finite element mesh of a standard shape geometry encompassing desired structure to be optimized in accordance with at least one design objective and orthotropic properties of material arising out of a selected material and selected additive manufacturing process to be used for manufacturing the designed structure;
    applying, at an application module, an iterative topology optimization of the designing structure, wherein each iteration of the topology optimization comprising of simulating one or more loading requirements, one or more design constraints and one or more boundary conditions under which the designing structure is designed and optimized;
    evaluating, at an evaluation module, the designing structure resulted from application of the iterative topology optimization using finite element analysis framework to obtain a predefined factor of safety based on the anisotropic properties of the material arising out of the selected additive manufacturing process, wherein the predefined factor of safety condition is defined as a substantially small difference in comparison with evaluated factor of safety;
    modifying, at a modification module, the state of the finite element iteratively according to one or more changes of the factor of safety between two consecutive iterations of the iterative topology optimization of the designing structure; and
    obtaining an optimal designing structure when the entire structure has a minimal factor of safety equivalent to a predefined factor of safety.
EP17203244.3A 2017-03-22 2017-11-23 A system and method for design of additively manufactured products Active EP3379434B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IN201721010130 2017-03-22

Publications (2)

Publication Number Publication Date
EP3379434A1 true EP3379434A1 (en) 2018-09-26
EP3379434B1 EP3379434B1 (en) 2022-09-28

Family

ID=60569581

Family Applications (1)

Application Number Title Priority Date Filing Date
EP17203244.3A Active EP3379434B1 (en) 2017-03-22 2017-11-23 A system and method for design of additively manufactured products

Country Status (3)

Country Link
US (1) US10885706B2 (en)
EP (1) EP3379434B1 (en)
JP (1) JP7061881B2 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111319268A (en) * 2020-02-20 2020-06-23 西北工业大学 Self-supporting structure optimization design method considering additive manufacturing printing direction
CN112395699A (en) * 2020-11-06 2021-02-23 广州理工学院 Preparation method of medical fixing brace based on topology optimization
CN112417692A (en) * 2020-11-24 2021-02-26 华东交通大学 Multi-scale topological optimization design method of material structure based on load uncertainty
CN112685945A (en) * 2021-01-11 2021-04-20 北京理工大学 Magnetic-structure multi-physical-field topological optimization design method for additive manufacturing
CN112966410A (en) * 2021-02-03 2021-06-15 西安交通大学 Additive manufacturing self-supporting structure topology optimization method suitable for variable critical angle
CN113657010A (en) * 2021-10-21 2021-11-16 山东神力索具有限公司 Meshing adjustment method and system for rigging model and electronic equipment
CN116776692A (en) * 2023-06-26 2023-09-19 小米汽车科技有限公司 Knuckle design optimization method and device, electronic equipment and storage medium

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017189064A1 (en) * 2016-01-29 2017-11-02 Massachusetts Institute Of Technology Topology optimization with microstructures
US11465356B2 (en) * 2017-06-20 2022-10-11 Toray Engineering Co., Ltd. Method for predicting strength of structure, method for modeling structure, support method for additive manufacturing of structure, and recording medium
US10073440B1 (en) * 2018-02-13 2018-09-11 University Of Central Florida Research Foundation, Inc. Method for the design and manufacture of composites having tunable physical properties
JP6962855B2 (en) * 2018-04-13 2021-11-05 株式会社日立製作所 Laminated model design support device and laminated model design support method
JP7058207B2 (en) * 2018-10-25 2022-04-21 Dmg森精機株式会社 Machine tool manufacturing method and manufacturing system
CN110103474B (en) * 2019-04-04 2021-03-26 同济大学 Part bionic structure additive manufacturing method based on stress regulation and control
CN110705153B (en) * 2019-09-24 2023-09-05 中国航空工业集团公司沈阳飞机设计研究所 Unmanned aerial vehicle multi-order safety coefficient value-taking method
JP7452110B2 (en) 2020-03-06 2024-03-19 富士フイルムビジネスイノベーション株式会社 Information processing device, three-dimensional shape data generation device, three-dimensional modeling device, and information processing program
CN111651811B (en) * 2020-04-13 2024-03-19 中建三局第一建设工程有限责任公司 Staged reverse design method for respiratory temporary infectious disease hospital assembled building system
CN111924331B (en) * 2020-07-16 2022-02-08 燕山大学 Method and system for optimizing vertical bracket structure in steel coil transportation and standing process
CN111783259B (en) * 2020-07-31 2024-03-29 徐州巴特工程机械股份有限公司 Safety assessment method for bucket structure
CN111985061B (en) * 2020-08-12 2023-03-28 上海电气风电集团股份有限公司 Structural design method and system of offshore wind turbine foundation and readable storage medium
CN112270048A (en) * 2020-11-17 2021-01-26 北京机电工程研究所 Structural topology optimization design method applied to equipment installation adaptor
CN112800655B (en) * 2021-02-02 2022-02-11 北京科技大学 Large and medium-sized part light weight design method based on generative optimization and guided reconstruction
TR2021003400A1 (en) 2021-02-26 2022-09-21 Tobb Ekonomi Ve Teknoloji Ueniverisitesi A topology optimization system.
CN113094943B (en) * 2021-03-15 2022-08-09 华中科技大学 Level set topology optimization method, system, device and medium

Family Cites Families (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030079188A1 (en) * 2001-10-17 2003-04-24 Analog Design Automation Inc. Method of multi-topology optimization
WO2007044277A2 (en) 2005-10-04 2007-04-19 Aztec Ip Company, L.L.C. Parametrized material and performance properties based on virtual testing
DE102005055825A1 (en) * 2005-11-23 2007-05-24 Basf Ag Sample`s particle individual, three dimensional form e.g. powder form, automated determining method, involves observing particles from two observation directions, where particle axis is aligned along line transverse to observation direction
US20080300831A1 (en) * 2006-12-19 2008-12-04 Board Of Governors For Higher Education, State Of Rhode Island And Providence System and method for finite element based on topology optimization
US8880380B2 (en) * 2007-12-21 2014-11-04 Honda Motor Co., Ltd. Crashworthiness design methodology using a hybrid cellular automata algorithm for the synthesis of topologies for structures subject to nonlinear transient loading
KR100989190B1 (en) * 2008-08-29 2010-10-20 한양대학교 산학협력단 Method for topology optimization design using equivalent static loads
US8126684B2 (en) * 2009-04-10 2012-02-28 Livermore Software Technology Corporation Topology optimization for designing engineering product
WO2013091085A1 (en) 2011-12-23 2013-06-27 The Royal Institution For The Advancement Of Learning/Mcgill University Bone replacement implants with mechanically biocompatible cellular material
CN104769592B (en) * 2012-11-06 2019-03-22 杰富意钢铁株式会社 Shape optimum analysis method and device
US20150054204A1 (en) * 2013-08-26 2015-02-26 Escape Dynamics Inc. Additive Manufacturing Microwave Systems And Methods
AU2015208658A1 (en) * 2014-01-24 2016-08-18 Rmit University Structured porous metamaterial
EP3137002A4 (en) * 2014-03-11 2018-06-20 The Ohio State Innovation Foundation Methods, devices, and manufacture of the devices for musculoskeletal reconstructive surgery
US9747394B2 (en) * 2014-03-18 2017-08-29 Palo Alto Research Center Incorporated Automated design and manufacturing feedback for three dimensional (3D) printability
US10061870B2 (en) * 2014-03-18 2018-08-28 Palo Alto Research Center Incorporated Automated metrology and model correction for three dimensional (3D) printability
US9946816B2 (en) * 2014-03-18 2018-04-17 Palo Alto Research Center Incorporated System for visualizing a three dimensional (3D) model as printed from a 3D printer
US20160096318A1 (en) * 2014-10-03 2016-04-07 Disney Enterprises, Inc. Three dimensional (3d) printer system and method for printing 3d objects with user-defined material parameters
TWI519987B (en) * 2014-11-14 2016-02-01 財團法人工業技術研究院 Structural topology optimization design method
US9895845B2 (en) * 2015-02-16 2018-02-20 Arevo Inc. Method and a system to optimize printing parameters in additive manufacturing process
US10227145B2 (en) * 2015-02-27 2019-03-12 Space Systems/Loral, Llc Truss structure
CN107949868A (en) * 2015-09-07 2018-04-20 西门子产品生命周期管理软件公司 Modeling method and system
JP6537216B2 (en) * 2015-12-03 2019-07-03 ザ・リージェンツ・オブ・ザ・ユニバーシティ・オブ・ミシガン Shape Optimization Using Reduced-Length Boundaries for Structural Segments of Different Thicknesses
WO2017189064A1 (en) * 2016-01-29 2017-11-02 Massachusetts Institute Of Technology Topology optimization with microstructures
JP7107852B2 (en) * 2016-05-24 2022-07-27 ダイバージェント テクノロジーズ, インコーポレイテッド Systems and methods for additive manufacturing of transportation structures
US10395372B2 (en) * 2016-06-28 2019-08-27 University Of Cincinnati Systems, media, and methods for pre-processing and post-processing in additive manufacturing
US10259044B2 (en) * 2016-06-29 2019-04-16 Velo3D, Inc. Three-dimensional printing and three-dimensional printers
US11062058B2 (en) * 2016-08-11 2021-07-13 Autodesk, Inc. Usage feedback loop for iterative design synthesis
US10353378B2 (en) * 2016-08-18 2019-07-16 Wisconsin Alumni Research Foundation Homogenization of material properties in additively manufactured structures
US11086294B2 (en) * 2017-04-12 2021-08-10 Autodesk, Inc. Combining additive and conventional manufacturing techniques to improve manufacturability

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
J. STEGMANN ET AL: "Discrete material optimization of general composite shell structures", INTERNATIONAL JOURNAL OF NUMERICAL METHODS IN ENGINEERING., vol. 62, no. 14, 1 January 2005 (2005-01-01), GB, pages 2009 - 2027, XP055410185, ISSN: 0029-5981, DOI: 10.1002/nme.1259 *
JIKAI LIU: "Guidelines for AM part consolidation", VIRTUAL AND PHYSICAL PROTOTYPING, vol. 11, no. 2, 2 April 2016 (2016-04-02), UK, pages 133 - 141, XP055482225, ISSN: 1745-2759, DOI: 10.1080/17452759.2016.1175154 *
PU ZHANG ET AL: "Role of anisotropic properties on topology optimization of additive manufactured load bearing structures", SCRIPTA MATERIALIA., vol. 135, 27 October 2016 (2016-10-27), NL, pages 148 - 152, XP055372441, ISSN: 1359-6462, DOI: 10.1016/j.scriptamat.2016.10.021 *
ROBERT M HOGLUND: "An Anisotropic Topology Optimization Method For Carbon Fiber-Reinforced Fused Filament Fabrication", 1 August 2016 (2016-08-01), Waco, TX, USA, pages i - 169, XP055482239, Retrieved from the Internet <URL:https://baylor-ir.tdl.org/baylor-ir/bitstream/handle/2104/9821/HOGLUND-THESIS-2016.pdf?sequence=1&isAllowed=y> [retrieved on 20180607] *

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111319268A (en) * 2020-02-20 2020-06-23 西北工业大学 Self-supporting structure optimization design method considering additive manufacturing printing direction
CN111319268B (en) * 2020-02-20 2021-12-28 西北工业大学 Self-supporting structure optimization design method considering additive manufacturing printing direction
CN112395699A (en) * 2020-11-06 2021-02-23 广州理工学院 Preparation method of medical fixing brace based on topology optimization
CN112417692A (en) * 2020-11-24 2021-02-26 华东交通大学 Multi-scale topological optimization design method of material structure based on load uncertainty
CN112685945A (en) * 2021-01-11 2021-04-20 北京理工大学 Magnetic-structure multi-physical-field topological optimization design method for additive manufacturing
CN112685945B (en) * 2021-01-11 2021-08-13 北京理工大学 Magnetic-structure multi-physical-field topological optimization design method for additive manufacturing
CN112966410A (en) * 2021-02-03 2021-06-15 西安交通大学 Additive manufacturing self-supporting structure topology optimization method suitable for variable critical angle
CN112966410B (en) * 2021-02-03 2022-12-09 西安交通大学 Additive manufacturing self-supporting structure topology optimization method suitable for variable critical angle
CN113657010A (en) * 2021-10-21 2021-11-16 山东神力索具有限公司 Meshing adjustment method and system for rigging model and electronic equipment
CN116776692A (en) * 2023-06-26 2023-09-19 小米汽车科技有限公司 Knuckle design optimization method and device, electronic equipment and storage medium
CN116776692B (en) * 2023-06-26 2024-02-23 小米汽车科技有限公司 Knuckle design optimization method and device, electronic equipment and storage medium

Also Published As

Publication number Publication date
US20180276889A1 (en) 2018-09-27
EP3379434B1 (en) 2022-09-28
JP7061881B2 (en) 2022-05-02
US10885706B2 (en) 2021-01-05
JP2018158570A (en) 2018-10-11

Similar Documents

Publication Publication Date Title
EP3379434B1 (en) A system and method for design of additively manufactured products
Altieri et al. Reliability-based optimal design of nonlinear viscous dampers for the seismic protection of structural systems
JP7177602B2 (en) Structural Optimization Method for Additively-manufactured Parts Considering States Induced by Additively-manufactured Parts
US20160147914A1 (en) Technique for generating approximate design solutions
Aremu et al. The effects of bidirectional evolutionary structural optimization parameters on an industrial designed component for additive manufacture
EP3864471B1 (en) Elastic strain engineering of materials
Ghaffari Motlagh et al. Deep learning phase‐field model for brittle fractures
JP7030064B2 (en) Systems and methods for material composition modeling
US11501037B2 (en) Microstructures using generative adversarial networks
Fish et al. A nonlocal multiscale fatigue model
US8078446B2 (en) Linear time-invariant system modeling apparatus and method of generating a passive model
Wang et al. Iterative learning control with complex conjugate gradient optimization algorithm for multiaxial road durability test rig
Zhao et al. Simulation and experimental validation of powertrain mounting bracket design obtained from multi-objective topology optimization
Werner et al. Multidisciplinary design optimization of a generic b-pillar under package and design constraints
US11409932B1 (en) C-PHY input/output driver modeling using artificial neural network and state space models
EP4016368A1 (en) Method for fast detection of unconstrained motion and low-stiffness connections in finite element modeling
US20180101632A1 (en) Computing system and method of performing verification of circuit design in the computing system
Huang et al. A modified gradient projection method for static and dynamic topology optimization
Li et al. Efficient modelling and optimization for double wishbone suspensions based on a non-adaptive sampling sparse response surface
Arjomandi Rad et al. Image regression-based digital qualification for simulation-driven design processes, case study on curtain airbag
US11599768B2 (en) Cooperative neural network for recommending next user action
Horibe et al. Quantitative measure for nonlinear unstable systems based on the region of attraction and its application to designing parameter optimization–inverted pendulum example
Messer et al. Model refinement decisions using the process performance indicator
WO2020068364A1 (en) Iterative solvers having accelerated convergence
Cerini et al. Estimation of a Craig–Bampton equivalent model using a hybrid particle swarm optimization for DCLA purposes

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20190326

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20210514

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

REG Reference to a national code

Ref country code: DE

Ref legal event code: R079

Ref document number: 602017062104

Country of ref document: DE

Free format text: PREVIOUS MAIN CLASS: G06F0017500000

Ipc: G06F0030170000

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

RIC1 Information provided on ipc code assigned before grant

Ipc: G06F 119/18 20200101ALN20220329BHEP

Ipc: G06F 30/17 20200101AFI20220329BHEP

INTG Intention to grant announced

Effective date: 20220412

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602017062104

Country of ref document: DE

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1521729

Country of ref document: AT

Kind code of ref document: T

Effective date: 20221015

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: NL

Ref legal event code: FP

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20221228

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1521729

Country of ref document: AT

Kind code of ref document: T

Effective date: 20220928

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20221229

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230130

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230128

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602017062104

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230526

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20221130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221123

26N No opposition filed

Effective date: 20230629

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221123

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20221130

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 20231124

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20231121

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20231123

Year of fee payment: 7

Ref country code: DE

Payment date: 20231127

Year of fee payment: 7

Ref country code: CH

Payment date: 20231201

Year of fee payment: 7

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20171123

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20220928